Page 322 - (KU)01-75GAJ-1.5 - Change 1

INTRO

EP'S (KU)01-75GAJ-1.5 FIGURES

Lost
Bus ‡ Defensive systems degraded: MWS system inoperative.
Com RWR ACAWS partially inoperative; monitor RWR ACAWS
failure performance. CMDS remote dispense switches at the
augment station and parachute doors inoperative. All
BYPASS mode functions inoperative. Tail dispenser GROUND
inoperative.
‡ Normal brake pressure may bleed off when setting
parking brake (parking brake valve will remain as-is). TAKEOFF
Ensure aircraft is chocked and use emergency brake
pressure for parking.
‡ Exterior lighting degraded: Leading edge and wing tip FIRE/SMK
NORM navigation lights inoperative. Landing lights will not
extend/ retract but will turn on. Consider destination
runway lighting conditions if landing at night. PRES/OXY
‡ HF 2 and ADF 2 inoperative.
F. BAU II #4 FAIL*...................................................... Review ENG/PROP

G. Fault Log................................................................ Review
FUEL
)$'(& % % 3523 $8; 3803
F/ODS CH B, R DUMP VLV, ADF 2, HF 2
LDG LTS RETRACT/EXTEND, LEADING EDGE LTS AAR
UTIL HYD SUCT PUMP, PARK BRAKE VALVE
ANTISKID
SPEC NOT FOR FLIGHT ELEC
OIL FLAP 2/3 RETRACT, OIL FLAP 3 EXTEND
MISSLE WARNING, ALE TAIL, HF 2 SECURE VOICE
BAU II #4 HYD
FUS TK XFER PUMP
SENSORS: FLT CTRL
CGO AIR COND FLOW CTRL VLV OUTLET
DUCT TEMP
FLOOR HEAT SUPPLY DUCT TEMP GEAR
CGO OVRHD RECIRC FAN DUCT PRESS
CGO TURBINE OUTLET DUCT PRESS DOR/RMP
PERF R BLD AIR CROSS-SHIP MANIFOLD DUCT
PRESS
(End of Procedure) JETTISON

Lost Bus Comm failure: If communications have failed, most ECBs stay
in their last state. LANDING

The ACAWS associated with a Lost Bus Comm failure are:
DITCHING
‡ ANTI-SKID FAIL (C) (when gear is down)

H. ANTI SKID switch....................................................................... OFF
BAILOUT

OPER FAULT LG

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